N431AW
Service difficulty reports · 254
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N431AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N431AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR A6WA201040088Attach Angle · crackedCRACKED ATTACH ANGLE UNDER PANEL 326C, PN 60021137-5. R & R IAW SRM.SDR A6WA201040087Angle · crackedCRACKED ATTACH ANGLE UNDER 326CL LT TOP SIDE OF VERT STAB PN 600-21137-5. DUPLICATE AND REPLACE IAW SRM.SDR A6WA201040090Angle · crackedRT OBLIQUE ANGLE CRACKED AT FS 625.0, R & R IAW SRM.SDR A6WA201040089Angle · crackedLT OBLIQUE ANGLE AT FS 625 CRACKED. R & R IAW SRM.SDR A6WA201040081Stiffener · crackedVERT STIFFENER AT RBL 9 CRACKED ON 559 PRESSURE BULKHEAD. REPLACED DURING REO 601R-53-41-260 INCORPORATION.SDR A6WA201040080Angle · crackedATTACH ANGLE AT INBD END OF WING L/E 530JL CRACKED (PN 600-12045-11).SDR A6WA200940814Structure · crackedNLG DOOR MECH BASE IS CRACKED AT LOWER AFT PIVOT OF HYD ACTUATOR RT SIDE. R & R RT SIDE NLG DOOR MECH ASSY. (K)SDR A6WA200940475Bulkhead · crackedEDDY CURRENT INSPECTION SHOWS STRONG DISCONINUITY INDICATION OF FWD FACE OF AFT PRESSURE BULKHEAD AT APPROX LBL 11.0 AND WL 116.0. INDICATION IS APPROX 0.5" IN LENGTH AND RUNS ROUGHLY VERTICALLY. EO 601R-53-61-3301, REV A AND GREO 601R-53-61-1285 TO REAR PRESDR A6WA200940201Check Valve · malfunctioned291717/3 -14TH STAGE BLEED AIR CHECK VALVE REMOVED FOR INSPECTION. FOUND BUTTERFLY VALVE PARTS MISSING. REF LOG 201715/1 - RT WING ANTI-ICE OVERHEAT. ENGINE NR 2, 14TH STAGE BLEED AIR CHECK VALVE REPLACED IAW AMM 30-12-01 MISSING PIECES FOUND IN REMOVED RT SDR A6WA200940172Piccolo Tube · damagedANTI-ICE DUCT WARNING MESSAGE IN FLIGHT WITH ANTI-ICE SELECTED ON. RT WING L/E SHOWED RED ON SYNOPTIC PAGE. REMOVED AND REPLACED RT OTBD PICCOLO TUBE IAW AMM 30-11-14. (K)SDR A6WA200940122Window · crackedTHE RT COCKPIT WINDOW CRACKED. REMOVED AND REPLACED F/O`S WINDOW IAW AMM 56-12-01. OPS AND LEAK CHECK GOOD. (K)SDR A6WA200940012Fitting · looseLOG 188378/2 AND 3 - ACFT LEAKING FUEL FROM AFT DRAIN MAST AT TAIL. ACFT SMELLS LIKE FUEL INSIDE CABIN. VERIFIED LEAK COMING FROM APU AND STOPPED WITH APU SHUTDOWN AND ODOR IN CABIN DISSAPATED, REF 188378/3 FOR MEL. RESECURED LOOSE FITTING BETWEEN FCU AND SSDR A6WA200940137Control Unit · failedA SKID IB CAUTION MSG ON GEAR EXTENSION. T/S IAW FIM 32-40-00, SHEET 7 BLK 9 ASCU BITE SKID CHECK W/N PASS, REMOVED AND REPLACED ASCU IAW AMM 32-44-06. OPS TEST GOOD. (K)SDR A6WA200840647Control Unit · malfunctionedLOG 188366/3 ANTI-SKID INBD CAUTION MSG ON GEAR EXTENSION. T/S PER FIM 32-40-00. ASCU BITE SKID CHECK W/N PASS, R&R ANTI-SKID CONTROL UNIT IAW AMM 32-44-06. OPS TEST GOOD.SDR A6WA200840540Flap System · out of rigAIRCRAFT ROLLS LT WITH THRUST, EVEN IN DESCENT AND CRUISE. APPROXIMATELY 50% TRIM RWD. CAPTAIN YOKE HAS FREE PLAY (LT AND RT), FIRST OFFICERS YOKE NORMAL. FLAPS FOUND OUT OF RIG. FLAPS HAVE BEEN RIGGED USING AMM 27-51-00. BOTH LT AND RT CONTROL WHEEL QUADSDR A6WA200840457Target · out of adjustGEAR DISAGREE LT MLG SHOWS HATCHED. COMPLIED WITH QRH, RETURNED TO PHL. SECURED LT MLG UPLOCK TARGET REF AMM 32-32-05, OPS CHECK AND GEAR SWINGS GOOD.SDR A6WA200840400Throttle · out of adjustUPON ENGINE SHUTDOWN, RIGHT ENGINE CONTINUED TO RUN WITH THRUST LEVER IN SHUTOFF POSITION. WORKED THROTTLE LEVER, ENGINE EVENTUALLY SHUTDOWN. ADJUSTED THROTTLE CONTROL RIGHT ENGINE IAW 76-11-17. PERFORMED IDLE SPEED CHECK IAW 70-00-00. OPS CHECK GOOD. (A)SDR A6WA200840335Fan · misinstalledCAPTAIN AND F/O RECEIVED DISPLAY TEMP MESSAGE ON PFD`S. BOTH ATTITUDE INDICATORS SHOW BLACK. FOUND COCKPIT DISPLAY COOL GROUND FAN CONNECTOR LOOSE. SECURED CONNECTOR AS REQUIRED. ALSO FOUND COCKPIT DISPLAY COOL FLIGHT FAN INSTALLED BACKWARDS. RE-INSTALLEDSDR A6WA200840333Warning Light · illuminatedDISPLAY COOL MSG IN FLIGHT, FOLLOWED QRH MSG STAYED ON IN STANDBY FAN POSITION DIVERTED TO PHL MSG WENT OUT INBOUND OF PHL AFTER 10-15 MINUTES. (M)SDR A6WA200840323Flap System · malfunctionedABORTED TAKEOFF DUE TO CONFIG FLAP WARNING. FLAP INDICATION SHOWED 3 DEGREES WHEN SELECTED TO 8 DEGREES. TAKEOFF ABORTED AT 60 KNOTS. BTMS INDICATED 3-3-5-3. INTERROGATED FECU PER AMM 27-50-00. NO DEFECTS NOTED. RESET FLAP SYSTEM IAW FIM PROCEDURES. OPSDR A6WA200840219Warning Light · false activationWING DUCT FAIL WARNING ON EICAS/WITH MASTER WARNING. COMPLIED WITH QRH. MESSAGE CLEARED. OPS CHECK OF WING ANTI-ICE GOOD IAW AMM 30-12-00. CHECKED RESISTANCE TO GROUND AT CONTROLLERS OF 14TH STAGE LEAK DETECTION SYSTEM, NO DEFECTS FOUND.SDR A6WA200840079Bulkhead · crackedPILOTS BULKHEAD WEB IS CRACKED AT FS 280.00, WL 85.00 LBL 27.00. (K) REPAIRED WEB IAW SRM 51-71-28 FIGURE 2. (M)SDR A6WA200840078Plate · corrodedSERVICE DOOR PLATE ASSY CORRODED. (K) SERVICE DOOR PLATE ASSY REPLACED.SDR A6WA200840081Cargo Track · corrodedAT FS 559.96 WL 73.50 CARGO TRACK LT AND RT SIDE INNER, OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12-00. (M)SDR A6WA200840080Cargo Track · corrodedAT FS 574.00, WL 73.50 CARGO TRACKS LT AND RT SIDE INNER OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12-00. (M)SDR A6WA200840077Support · crackedAC GROUND POWER RECEPTACLE SUPPORT MEMBER IS CRACKED. (K) SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M)SDR A6WA200840075Plate · corrodedTWO CRACKS ON FLOOR LANDING PLATE AT FS 589 AND FS 605. (K) REPAIRED IAW REO 601R-53-61-433. (M)SDR A6WA200840074Plate · corrodedFLOOR LANDING PLATE CORRODED BETWEEN FS 559 + 112 TO FS 621, AROUND NUT PLATE HOLES. (K) CORROSION ON FLOOR LANDING PLATE BETWEEN FS 559 PLUS 112 TO FS 621 AROUND NUT PLATE HOLES, BENDED IAW SRM 51-21-06. (M)SDR A6WA200840076Floor Support · corrodedFLOOR SUPPORT CORRODED AT FS 589.0 TO 605.0 NL 73.50 LBL 10.0. (K) REPAIRED IAW REO 601R-53-00-027 REV C. (M)SDR A6WA200740546Oil System · lowAPU OIL CAUTION MESSAGE IN FLIGHT. SERVICED APU OIL IAW AMM 12-13-49. ADDED 1 PINT. PERFORMED, OPS TEST OF APU IAW 49-10-01, OPS CHECK GOOD. (M)SDR A6WA200740312Push-Pull Rod · out of positionPASSENGER DOOR WILL NOT OPEN/CLOSE FROM OUTSIDE. OPCV NORMAL FROM INSIDE. PLACARDED AND PLACED ON MEL. REPOSITIONED OUTER DOOR HANDLE PUSHPULL TUBES IAW CMM. OPS CHECK GOOD. REMOVED FROM MEL. (K)SDR A6WA200640367A/C Pack · malfunctionedLEFT PACK HIGH PRESSURE, YELLOW AMBER CAUTION MESSAGE ON TAKEOFF. ABORTED TAKEOFF BELOW 80 KNOTS (30 KNOTS), MAX BTMS READING 3, TAKEOFF WEIGHT 44,000 LBS. PLACARDED AND PLACED ON MEL, NO RTO/HES INSPECTION REQUIRED. REMOVED AND REPLACED PRESSURE SWITCH S1HSDR A6WA200640295Rib · crackedRIGHT WING BATT RIB IS CRACKED 1 INCH ALONG TOP AFT CORNER AT WS 53.60. MAINTENANCE TRIMMED OUT CRACK, INSTALLED FILLER AND REPAIR ANGLE IAW REO 601R-57-51-046 REV B. (M)SDR A6WA200640296Rib · crackedFOUND LEFT WING BATT RIB IS CRACKED 1 INCH LONG AT TOP AFT CORNER. MAINTENANCE REPAIRED LEFT WING BATT RIB ASSEMBLY IAW REO 601R-57-51-046 REPAIR NR 2. (M)SDR A6WA200640272Torque Tube · out of adjustMAIN PASSENGER DOOR WOULD NOT OPEN WITH PASSENGERS ONBOARD. FUNCTION NORMAL WITH AIRCRAFT EMPTY.. PLACARDED AND PLACED ON MEL. COMPLIED WITH INSPECTION AND FUNCTION CHECK OF PASSENGER DOOR IAW AMM. PERFORMED ADJUSTMENT OF UPPER TORQUE TUBE IAW AMM. OPS CHSDR A6WA200640270Handle · dirtyPAX DOOR WILL NOT OPEN. CLEANED PAX DOOR HANDLE ASSY AND LUBED SHOOT BOLTS PER AMM CHAPTER 12, PAX DOOR CHECKS GOOD PER AMM CHAPTER 52. (M)SDR A6WA200640266Motor · failedUNABLE TO OPEN PAX DOOR INTERNALLY OR EXTERNALLY. INSPECTED AND FOUND PAX DOOR ASSIST CABLE NOT RETRACING AND TANGLED INHIBITING DOOR FROM OPENING. REPLACED ASSIST MOTOR IAW 52-11-08. (M)SDR A6WA200640240Psu · dislodgedPSU IN ROW 6 AND 7 LEFT SIDE INOPERATIVE, FELL DOWN. CREW DECLARED EMERGENCY AND COMPLIED WITH EMERGENCY LANDING. REPLACED SILICONE CHORD ON ON LT PSU AT ROW 6 AND 7 IAW CRJ AMM 25-28-01. (M)SDR A6WA200540327Aileron · unknownREQUEST INSPECTION OF RT AND LT AILERONS. THAWED ICE FROM AILERON, INSPECTED SURFACE MOVEMENT AND SURFACES. NO DEFECTS NOTED. (K)SDR A6WA200540222Smoke Detector · malfunctionedSMOKE CARGO MESSAGE AFTER PUSHBACK, GROUND INSPECTION OF CARGO HOLD. NO SMOKE FOUND. MEL`D NR 1 CARGO SMOKE DETECTOR. REMOVED AND REPLACED CARGO SMOKE DETECTOR. OPS CHECK GOOD IAW CRJ MM 26-15-00. REMOVED OFF MEL. S/N OFF 1719, S/N ON 2222. (M)SDR A6WA200540147Check Valve · stickingLOW OIL ENGINE PRESSURE WARNING IN FLIGHT (RED). INDICATED LOW ON GAUGE LOW PRESSURE, COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. REMOVED AND REPLACED ENGINE NR 2 GEARBOX BB CARBON SEAL AND MATING RING. ALSO, REMOVED AND REPLACED ENGINE NR 2 REPLENISHMENTSDR A6WA200540139Engine · malfunctionedLOW OIL ENGINE PRESSURE WARNING. INDICATED LOW ON GAGE LOW PRESSURE. COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. (M)SDR A6WA200540076Strut · dischargedAFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. SERVICED HYDRAULIC FLUID AND NITORGEN TO THE NOSE STRUT. ADJUSTED THE NOSE OLEO CENTER EXTEND SENSOR WITHIN LIMITS. (M)SDR A6WA200440139Acm · odorVERY STRONG ACRID SMELL COMING FROM AIR CONDITIONING PACKS. GOT WORSE WHEN TEMP CHANGES. REMOVED AND REPLACED LEFT ACM IAW AMM 21-51-10. (M)SDR A6WA200440073Frame · crackedFRAME FLANGE BETWEEN STRINGER 11-12 HAS A CRACK COMING FROM A RIVET HOLE. TRIMMED OUT CRACKED PORTION OF FRAME FLANGE. PERFORMED LPI OF CUTLINE TO ENSURE NO CRACKS EXIST. FABRICATING REPAIR FLANGE FROM FRAME SECTOR PN 600-36030-23 INSTALLED IAW REO 601R-53-SDR A6WA200440091Floorbeam · crackedFOUND FLOORBEAM ANGLES CRACKED AT FS 280, WL 73.50, LBL 9 AND RBL 9, FLOOR LEVEL. REMOVED OLD FLOOR SUPPORT ANGLES AT FS 280 WL 73.50 INBOARD SIDE OF LBL 9 AND RBL 9. INSTALLED NEW ANGLES PART NR RH 601R31113-58, LH 601R31113-57. ALL WORK IAW CRJ200 SRM 51-SDR A6WA200440071Floor Support · crackedFLOOR SUPPORT ANGLES CRACKED AT FS 280, WL 73.5 LBL 9 AND RBL 9, BOTH INBOARD ANGLES. REMOVED LEFT ANGLE, P/N 601R31113-57 AND RT ANGLE P/N 601R31113-58 AND INSTALLED NEW SAME P/N ANGLES LEFT AND RT AND TREATED AND PAINTED. ALL WORK PERFORMED IAW SRM 51-23-0SDR A6WA200440072Floorbeam · crackedFLOOR ANGLE AT FS 484, RBL 27 RIGHT INBOARD IS CRACKED. REMOVED CRACKED RT INBOARD FLOOR ANGLE AT FS 484 WL 73.5 AND FABRICATED NEW ANGLE FROM S6144-14 AND INSTALLED IAW REPAIR NUMBER 601R-53-0029. (M)SDR A6WA200340203Smoke Detector · false indicationCARGO SMOKE WARNING, FIRE BOTTLES BLOWN, WHILE AIRCRAFT ON GROUND WITH CARGO AND PASSENGER DOOR OPENED. INSPECTED CARGO COMPARTMENT, NO HEAT OR SMOKE DAMAGE. COMPLIED WITH MAINTENANCE ACTION TASK 26-15-00-040-801. DEACTIVATED BOTH CARGO SMOKE DETECTORS. REMSDR A6WA200340193Control Unit · malfunctionedTAT PROBE HEAT CAUTION ILLUMINATED INFLIGHT AFTER TAKEOFF. REPLACED AIR DATA HEAT SENSOR CONTROL UNIT. (M)
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